US11351612B2 - Manufacturing support and method for additive manufacturing process - Google Patents
Manufacturing support and method for additive manufacturing process Download PDFInfo
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- US11351612B2 US11351612B2 US16/419,519 US201916419519A US11351612B2 US 11351612 B2 US11351612 B2 US 11351612B2 US 201916419519 A US201916419519 A US 201916419519A US 11351612 B2 US11351612 B2 US 11351612B2
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- additive manufacturing
- body portion
- pillar
- metallic material
- cap portion
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/10—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of articles with cavities or holes, not otherwise provided for in the preceding subgroups
- B22F5/106—Tube or ring forms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/10—Processes of additive manufacturing
- B29C64/141—Processes of additive manufacturing using only solid materials
- B29C64/153—Processes of additive manufacturing using only solid materials using layers of powder being selectively joined, e.g. by selective laser sintering or melting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/30—Process control
- B22F10/38—Process control to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures
- B22F10/385—Overhang structures
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/40—Structures for supporting workpieces or articles during manufacture and removed afterwards
- B22F10/47—Structures for supporting workpieces or articles during manufacture and removed afterwards characterised by structural features
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/40—Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y40/00—Auxiliary operations or equipment, e.g. for material handling
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y50/00—Data acquisition or data processing for additive manufacturing
- B33Y50/02—Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/30—Process control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/60—Treatment of workpieces or articles after build-up
- B22F10/66—Treatment of workpieces or articles after build-up by mechanical means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y30/00—Apparatus for additive manufacturing; Details thereof or accessories therefor
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Definitions
- Various embodiments of the present disclosure relate generally to additive manufacturing and, more particularly, to manufacturing supports for additive manufacturing processes.
- Additive manufacturing can be employed to create a variety of parts, including mock-ups, prototypes, components of an assembly, or fully-functional devices.
- the term “additive manufacturing” encompasses a variety of manufacturing processes that involve constructing a part in a layer-by-layer manner.
- One type of additive manufacturing, powder bed fusion involves fusing grains of material together to form a part.
- Suitable materials for powder bed fusion processes may include polymeric or metallic powder.
- Laser sintering or electron beam melting may be employed to fuse particles of the powder together. Unsintered powder can be removed at the end of the process, leaving only the fused polymer or metal.
- Powder bed fusion processes may include depositing a layer of metal powder with a distributing mechanism such as a wiper or a roller, and fusing a portion of the deposited layer with a laser.
- manufacturing support structures with a box shape have been used.
- box-shaped manufacturing support structures may involve the use of large additional quantities of sintered material, add significantly to printing time, and form sharp edges that can damage the roller.
- alternative manufacturing support structures that reduce the size of the lattice and/or eliminate sharp edges may improve the manufacturing process.
- the hybrid support system disclosed in the '234 publication includes a volume support structure, a partially solidified support structure, and a reinforcement support structure.
- This hybrid support system is formed as a network of solid volume supports that are provided below the partially solidified support. While the support system disclosed in the '234 publication may be useful for supporting some types of parts, it may not be beneficial for parts in which precision is required. For example, the partially solidified portion may be difficult to separate from the part and may include unsupported regions that introduce deformations during the manufacturing process.
- the disclosed method, computer-readable storage medium, and pillar may solve one or more of the problems set forth above and/or other problems in the art.
- the scope of the current disclosure, however, is defined by the attached claims, and not by the ability to solve any specific problem.
- an additive manufacturing method for a part may include forming a pillar by fusing metallic material to form a hollow body portion including a wall having an inner surface and an outer surface and fusing metallic material to form a cap portion extending from a distal end of the body portion.
- the method may include forming the pillar by fusing metallic material to form a distal portion supported on the cap portion, supporting at least a portion of the part by the pillar, and removing the pillar from the part.
- a computer-readable storage medium may store instructions that, when executed by an additive manufacturing apparatus, cause the additive manufacturing apparatus to perform a method including forming a pillar by fusing metallic material to form a hollow body portion including a wall having an inner surface and an outer surface.
- the method may also include fusing metallic material to form a cap portion extending from a distal end of the body portion and fusing metallic material to form a distal portion supported on the cap portion.
- the method may additionally include fusing metallic material to form at least a portion of a part supported on the pillar.
- a pillar for supporting a part manufactured in an additive manufacturing process may include a hollow body portion including a wall having an inner surface and an outer surface, the wall including fused metallic material, a cap portion extending from a distal end of the body portion, and a distal portion supported on the cap portion.
- FIG. 1 is a schematic front view of an additive manufacturing system and a support pillar according to an aspect of the present disclosure.
- FIG. 2 is a front view showing the pillar of FIG. 1 according to an aspect of the present disclosure.
- FIGS. 3A, 3B, and 3C are cross-sectional views along lines 3 A- 3 A, 3 B- 3 B, and 3 C- 3 C, respectively, of FIG. 2 .
- FIG. 4 is a flowchart illustrating a method according to aspects of the present disclosure.
- FIG. 1 is a schematic front view of an additive manufacturing system 10 that may form an enclosed space in which a part 80 may be produced.
- Manufacturing system 10 may be a powder bed fusion device such as a selective laser sintering device.
- system 10 may include a platform or part bed 110 , a pair (or more) powder beds 120 on opposite sides of part bed 110 , and a controller 100 .
- Additive manufacturing system 10 may also include a heating device such as energy source 112 , which may be operably connected to a power supply 114 .
- a leveler 14 may be provided within system 10 and movable across powder beds 120 and part bed 110 .
- Controller 100 may be in communication with leveler 14 , part bed 110 , energy source 112 , power supply 114 , and powder bed 120 .
- Powder bed 120 may contain a reservoir of powder material 130 .
- Powder 130 may be any suitable powder material for additive manufacturing via melting or sintering such as polymeric or metallic powder.
- energy source 112 may be any suitable energy source configured to provide an energy beam such as a laser. In order to direct a beam of energy, energy source 112 may be included in an assembly including a mirror (not shown).
- Leveler 14 may be formed as one or more rollers configured to distribute powder. Leveler 14 be translateable across beds 110 , 120 in response to commands output by controller 100 . Leveler 14 may include, in addition to or in place of a roller, a wiper leveler (e.g., a rectangular wiper including a blade), or any other suitable leveler that is shaped so as to evenly distribute powder 130 .
- a wiper leveler e.g., a rectangular wiper including a blade
- Part 80 may include one or more overhanging portions 82 that, if left unsupported during the manufacturing process, may potentially cause deformation due to their weight.
- Overhanging portion 82 may, for example, have a mass that is not sufficiently supported by unsintered (loose) powder 130 that rests under portion 82 , as exemplified by part 80 on the right portion of bed 110 .
- a manufacturing support structure such as pillar 12 may rest on part platform 110 under overhanging portion 82 . Pillar 12 may be manufactured by system 10 during the manufacture of part 80 .
- Controller 100 may be, for example, any suitable computer or other device configured to receive and/or generate a file representing a part and control the various components of system 10 to construct the part 80 .
- controller 100 may be configured to control leveler 14 , part bed 110 , energy source 112 , and powder bed 120 to form a part provided via computer-aided design (CAD) software.
- CAD computer-aided design
- controller 100 may be configured to execute instructions provided on a storage medium such as computer-readable storage medium 102 .
- Computer-readable storage medium 102 may include, for example, magnetic storage including floppy disk, hard disk, or magnetic tape; semiconductor storage such as solid state disk (SSD) or flash memory; optical disc storage; magneto-optical disc storage; or any other type of physical memory on which information, a three-dimensional model, or other instructions readable by at least one processor may be stored.
- This storage medium 102 may store instructions configured to be executed by one or more processors of controller 100 to manufacture, or fabricate, part 80 and pillar 12 . These instructions may be generated via CAD software or other appropriate software. Alternatively, the instructions may be transmitted electronically to the controller 100 in a streaming fashion without being permanently stored at the location of the system 10 .
- Controller 100 may be configured to output control signals to movable platforms within powder beds 120 to direct powder 130 to an upper surface thereof and toward leveler 14 . Controller 100 may output control signals to power the energy source 112 via power supply 114 and direct the energy to desired locations of a layer of powder 130 on part bed 110 . Controller 100 may also control movement of part bed 110 and leveler 14 via respective motors (not shown). In an alternative configuration, additive manufacturing system 10 may be provided as an arc additive manufacturing system configured to fuse material provided as a wire.
- FIG. 2 is a front view showing an exemplary part 80 and a plurality of pillars 12 supporting respective overhanging portions 82 of part 80 .
- Part 80 may be a part having any desired shape, and may be produced based on a three-dimensional model (e.g., a digital file such as a solid model file or stereolithography (STL) file) provided to controller 100 .
- the model may be converted into a plurality of slices, for example substantially two-dimensional slices, that each define a cross-sectional layer of the part 80 . Pillar 12 may similarly be produced based on a three-dimensional model.
- Pillar 12 may include a hollow body portion 20 , a cap portion 40 , and a bridge or distal portion 60 that may provide a bridge between cap portion 40 and overhanging portion 82 . Each of these portions of pillar 12 may be formed as a single monolithic structure via the additive manufacturing process.
- Body portion 20 may extend from a proximal end 22 to a distal end 24 .
- Proximal end 22 may form a bottom of pillar 12 and is closest to and/or resting on part bed 110 .
- a through-hole may extend through an outer surface and inner surface of pillar 12 at proximal end 22 to form a drain hole 26 . While one drain hole 26 is shown in each pillar 12 in FIG. 2 , two, three, or more drain holes may be provided.
- Body portion 20 may form a hollow interior of pillar 12 that extends continuously from proximal end 22 to distal end 24 .
- “hollow” includes structures that contain unsintered powder or other loose material, air, other gases, etc.
- a “hollow” interior may be an interior that does not include fused metal powder.
- any loose powder may be drained via drain holes 26 .
- Distal end 24 of body portion 20 may support cap portion 40 at a distal end of the hollow interior.
- Cap portion 40 may cover or extend across a portion or all of distal end 24 . In one aspect, cap portion 40 may cover an entirety of distal end 24 and form an upper closed end of the hollow interior.
- Cap portion 40 may be formed by one or more inclined walls that gradually converge in a direction distal from body portion 20 .
- cap portion 40 may be formed by a pair of inclined walls ( FIG. 3B ) that gradually converge or taper in a distal direction.
- cap portion 40 may extend at an incline from distal portion 24 to a top distal ridge 46 ( FIG. 3B ).
- inclined walls of cap portion 40 may extend at an angle of 35 degrees or more with respect to a horizontal direction.
- cap portion 40 may have a greatest width at a proximal portion which is formed integrally with may distal end 24 of body portion 20 .
- Cap portion 40 may have a continuously narrowing width that terminates at a narrowest end formed by distal ridge 46 .
- a width of cap portion 40 may narrow in a direction distal from body portion 20 .
- distal portion 60 may include a plurality of individual members 62 that are fused together and form an irregular outer surface.
- the individual members 62 may include a tapering distal end 64 that is formed integrally with overhanging portion 82 . This tapering end 64 may facilitate separation of distal portion 60 from overhanging portion 82 and removal of pillar 12 from part 80 .
- Individual members 62 or groups of members 62 may extend by different amounts in a substantially vertical direction.
- distal portion 60 may include a series of peaks and valleys at the intersection of overhanging portion 82 and a distal end of distal portion 60 .
- Distal portion 60 may be formed as a lattice structure (e.g., a regular or an irregular pattern of nodes and struts or beams such as a honeycomb structure), cone-shaped (e.g., frustoconical) members, cylindrical members, members that together form a block-shape, and/or a plurality of sheet-shaped elements.
- a lattice structure e.g., a regular or an irregular pattern of nodes and struts or beams such as a honeycomb structure
- cone-shaped (e.g., frustoconical) members e.g., frustoconical) members
- cylindrical members e.g., cylindrical members that together form a block-shape, and/or a plurality of sheet-shaped elements.
- Pillar 12 may be provided with a height necessary to support overhanging portion 82 .
- the pillars 12 may have different respective heights.
- an overall height of pillar 12 may be defined by a distance from proximal end 22 of base portion 20 to a distal end of distal portion 60 .
- a height of body portion 20 may be greater than a height of cap portion 40 and a height of distal portion 60 .
- a height of body portion 20 may be greater than a combined height of cap portion 40 and distal portion 60 .
- a height of body portion 20 may be greater than 50% of the total height of pillar 12 .
- the height of body portion 20 may be greater than 75% of the total height of pillar 12 . In an exemplary configuration, the height of body portion 20 may be greater than 85% of the total height of pillar 12 .
- the size (e.g., width), of pillars 12 may also vary as necessary according to the shape of part 80 . In one aspect, a height of each pillar 12 may correspond to a height of the overhanging portion 82 , while a width of each pillar 12 may correspond to a width of overhanging portion 82 . In an exemplary configuration, a size (width) of pillar 12 may be about 85% or more of the size (width) of overhanging portion 82 . Pillar 12 may have a width that is less than a width of portion 82 . If desired, a plurality of pillars 12 may together support a single portion 82 .
- FIG. 3A is a cross-sectional view along line 3 A- 3 A of FIG. 2 illustrating body portion 20 .
- Body portion 20 may be defined by wall 28 which extends so as to define a continuous outer surface 30 and an opposite inner surface 32 .
- a hollow interior 34 of pillar 12 may extend throughout body portion 20 , and may be enclosed by wall 28 , except where a drain hole 26 is present.
- Outer surface 30 may form a substantially smooth, at least partially curved surface that is free or substantially free of any sharp edges.
- the at least partially curved surface of outer surface 30 may have a shape that generally corresponds to a shape of overhanging portion 82 . Particularly, outer surface 30 may be formed free of vertically-extending sharp edges.
- a vertically-extending edge is an edge of a portion of a manufacturing support that may face a surface of leveler 14 ( FIG. 1 ).
- a sharp edge may be formed by the intersection of two surfaces without the presence of a curve. Additionally, the lack of a sharp edge may be measured with respect to a vertical direction.
- outer surface 30 may be free of horizontally-extending edges such as edges that form a small angle with respect to a vertical direction.
- Wall 28 may have an approximately constant thickness. This thickness may, for example, be in the range of about 0.3 mm. to about 2 mm. In one aspect, the thickness of wall 28 may be between about 0.3 mm. to about 1 mm. Such thicknesses of wall 28 may provide adequate support for each portion of pillar 12 as well as for the overhanging portion 82 of part 80 , while requiring less material as compared to a support formed entirely of a lattice structure. If desired, wall 28 may be a lower-density wall in which every other layer is sintered, for example. Such a configuration of wall 28 may also have a thickness in a range of about 0.3 mm. to about 2 mm.
- FIG. 3B is a cross-sectional view along line 3 B- 3 B of FIG. 2 with part 80 omitted.
- FIG. 3B illustrates a portion of distal portion 60 and cap portion 40 .
- Cap portion 40 may extend distally from an outer periphery of body portion 20 at a lowest (most-proximal) end of cap portion 40 .
- a width defined by cap portion 40 at a most-proximal portion thereof may be approximately the same as the width of the corresponding portion of body portion 20 .
- Cap portion 40 may include a pair of inclined walls 42 , 44 provided on opposite sides of cap portion 40 .
- inclined walls 42 , 44 may be provided on opposite sides with respect to a major axis formed by body portion 20 .
- walls 42 , 44 may have a thickness that is approximately the same as the thickness of wall 28 of body portion 20 .
- Walls 42 , 44 may meet at a highest (most-distal) portion of cap portion 40 to form distal ridge 46 .
- inclined walls 42 , 44 and distal ridge 46 may form a support for distal portion 60 .
- distal portion 60 may have an outer circumferential shape that generally matches a circumferential shape of body portion 20 . While the shape of portions 20 and 60 may be similar, a width of distal portion 60 may be smaller than a width of body portion 20 .
- FIG. 3C is a cross-sectional view along line 3 C- 3 C of FIG. 2 with part 80 omitted.
- FIG. 3C illustrates a portion of distal portion 60 , including a plurality of members 62 .
- Adjacent members 62 of distal portion 60 may be fused together, or may form thin columns that are separated from each other. In an alternate configuration, members 62 may form a honeycomb shape.
- distal portion 60 may have an approximately uniform width, except at tapering ends 64 .
- Pillar 12 may be employed in a variety of additive manufacturing devices and processes.
- pillar 12 may be employed in any additive manufacturing process in which a part requires support, regardless of the size, shape, or intended use of the part. Pillar 12 may be especially useful for additive manufacturing processes that involve a process of fusing together metal particles and distributing metal particles with a leveler.
- Part 80 and pillar 12 may be formed in a layer-by-layer manner by additive manufacturing system 10 , for example.
- an amount of unsintered powder 130 may be pushed, via powder bed 120 , to a position in front of leveler 14 .
- Leveler 14 may then distribute the powder uniformly over part bed 110 to provide an upper layer of unsintered powder 130 , as shown in FIG. 1 .
- Energy source 112 may direct a beam of energy towards regions of this layer of powder 130 on bed 110 to melt or sinter precisely-defined regions of the upper layer of powder 130 , forming a portion of part 80 and/or pillar 12 by fusing material.
- another amount of unsintered powder 130 may be provided by a powder bed 120 and distributed by leveler 14 .
- additive manufacturing system 10 may fuse material such as a wire of material (e.g., in an arc additive manufacturing system).
- FIG. 4 illustrates an exemplary method 400 for producing a manufacturing support according to aspects of the present disclosure.
- Method 400 may be performed by executing instructions stored on computer-readable storage medium 102 , for example.
- a digital file representing a part such as part 80 may be provided to controller 100 prior to the performance of method 400 .
- metallic material such as powder may be fused such as by laser sintering, for example, to form hollow body portion 20 of pillar 12 . This may be performed by repeating a process of distributing and fusing layers of unsintered powder 130 .
- the body portion 20 of pillar 12 formed in step 402 may be supported on part bed 110 or on a portion of part 80 .
- Step 404 may include fusing metallic material such as powder 130 to form cap portion 40 .
- Step 402 may be performed following the completion of step 402 as cap portion 40 may be integrally formed on a distal end 24 of body portion 20 .
- cap portion 40 may be formed by distributing and fusing unsintered powder 130 at sequential positions above body portion 20 . Layers of fused powder 130 may form generally converging walls (e.g., walls 42 , 44 ) during the process of forming cap portion 40 .
- Step 404 may conclude when distal ridge 46 of cap portion 40 is completely formed.
- Step 406 may include fusing metallic material such as powder 130 to form distal portion 60 and may at least partially overlap with step 404 .
- distal portion 60 may begin to be formed on an upper surface of cap portion 40 .
- step 408 a portion of overhanging portion 82 may be formed on a distal region of distal portion 60 .
- step 408 may include fusing a portion of part 80 to pillar 12 .
- Step 406 may overlap with step 408 based on the geometry of the part 80 being manufactured.
- step 408 may be performed by forming overhanging portion 82 on distal portion 60
- the overhanging portion 82 may be supported by pillar 12 .
- a force of the weight of overhanging portion 82 which may increase with each subsequent layer of overhanging portion 82 , may be transmitted via distal portion 60 to cap portion 40 .
- the inclined walls 42 , 44 may transmit this force to the wall 28 of hollow body portion 20 .
- pillar 12 may support overhanging portion 82 by transmitting the force of the weight of overhanging portion 82 through each portion of pillar 12 .
- This weight may be uniformly distributed, maximizing the amount of weight pillar 12 can safely support, while eliminating the need to include a reinforcing structure within hollow interior 34 .
- Step 412 may be performed following the completion of each of steps 402 , 404 , 406 , and 408 .
- Distal portion 60 may be formed with a shape, such as tapering end 64 of members 62 , that facilitates removal from overhanging portion 82 of part 80 .
- one or more appropriate tools may be used to separate distal portion 60 from portion 82 .
- a tool such as a cold chisel may readily separate distal portion 60 from portion 82 .
- Any appropriate tool may be used to separate distal portion 60 and portion 82 .
- a surface of overhanging portion 82 may be polished or otherwise treated following the removal of distal portion 60 .
- the foregoing exemplary series of steps for performing method 400 may produce one of a plurality of pillars 12 .
- method 400 may be performed at each location that will provide support to overhanging portion 82 .
- Pillar 12 may provide improved strength with a reduced amount of material. Thus, pillar 12 may provide improved support and avoid deformation. Pillar 12 may therefore be especially beneficial when manufacturing tall parts, or parts with large overhanging portions.
- the use of a hollow body with a thin wall reduces the amount of material required to produce pillar 12 , significantly reducing cost and time necessary to produce a part. In one example, manufacturing time may be reduced by 30% or more.
- the lack of sharp edges may reduce wear or damage to the leveler 14 , whether in the form of a roller or a wiper. Thus, tall parts may be manufactured with reduced chance of creating tears or cuts in the leveler.
- the form of pillar 12 may also reduce the likelihood that the support structure itself becomes deformed or damaged, which may cause a manufacturing process to fail.
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- Physics & Mathematics (AREA)
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Abstract
Description
Claims (20)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/419,519 US11351612B2 (en) | 2019-05-22 | 2019-05-22 | Manufacturing support and method for additive manufacturing process |
| CN202010388762.9A CN111974993B (en) | 2019-05-22 | 2020-05-09 | Manufacturing support and method for additive manufacturing process |
| DE102020112882.7A DE102020112882A1 (en) | 2019-05-22 | 2020-05-12 | MANUFACTURING AID AND METHODS FOR ADDITIVE MANUFACTURING METHODS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16/419,519 US11351612B2 (en) | 2019-05-22 | 2019-05-22 | Manufacturing support and method for additive manufacturing process |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20200368814A1 US20200368814A1 (en) | 2020-11-26 |
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| Publication number | Publication date |
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| US20200368814A1 (en) | 2020-11-26 |
| CN111974993B (en) | 2024-09-03 |
| CN111974993A (en) | 2020-11-24 |
| DE102020112882A1 (en) | 2020-11-26 |
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